Low coefficient of expansion rotors for vacuum boosters
A vacuum booster assembly includes, but is not limited to, a booster housing defining a booster chamber and including a gas inlet and a gas outlet; a first rotor positioned within the booster chamber and adapted for rotation therein, the first rotor including a first shaft and at least two lobes defining a first lobe profile; and a second rotor positioned within the booster chamber and adapted for rotation therein, the second rotor including a second shaft and at least two lobes defining a second lobe profile, wherein the first and second rotors are formed from a metal having a coefficient of thermal expansion from about 1 (10 −6 in/in*K) to about 13 (10 −6 in/in*K), and wherein at least one of the outer surface of the first rotor, the outer surface of the second rotor, or the booster chamber includes a coating.
1. A vacuum booster assembly comprising:
a booster housing defining a booster chamber, the booster housing formed to include a gas inlet for allowing gas to enter the booster chamber and a gas outlet to allow gas to exit the booster chamber;
a first rotor positioned within the booster chamber and adapted for rotation therein, the first rotor including a first shaft and at least two lobes having an outer surface that defines a first lobe profile; and
a second rotor positioned within the booster chamber and adapted for rotation therein, the second rotor including a second shaft and at least two lobes having an outer surface that defines a second lobe profile,
wherein the first and second rotors are formed from a metal having a coefficient of thermal expansion from about 1 (10 −6 in/in*K) to about 13 (10 −6 in/in*K), wherein the outer surface of the first rotor and the outer surface of the second rotor each includes a coating including at least one of an abradable coating or a formable coating, and wherein a portion of the coating has a thickness from about 0.001 inches to about 0.025 inches and a surface roughness from about 125 Ra to about 1000 Ra.
2. The vacuum booster assembly of claim 1 , wherein the coefficient of thermal expansion of the first and second rotors is from about 6 (10 −6 in/in*K) to about 11 (10 −6 in/in*K).
3. The vacuum booster assembly of claim 2 , wherein the portion of the coating has a thickness from about 0.001 inches to about 0.006 inches.
4. The vacuum booster assembly of claim 1 , wherein the coating includes at least two layers formed from two different materials.
5. The vacuum booster assembly of claim 1 , wherein the portion of the coating from the first and second rotors partially transfers onto a portion of the booster housing during operation of the vacuum booster assembly.
6. The vacuum booster assembly of claim 1 , including an operating clearance between the first and second rotors from about 0.003 inches to about 0.032 inches and an operating clearance between the first rotor and the housing from about 0.002 inches to about 0.025 inches.
7. The vacuum booster assembly of claim 1 , wherein the coating has a coefficient of friction from about 0.04μ to about 0.2μ.
8. The vacuum booster assembly of claim 1 , wherein the coating includes one or more of a PTFE, a graphite, or molybdenum disulfide.
9. A vacuum booster assembly comprising:
a booster housing defining a booster chamber, the booster housing formed to include a gas inlet for allowing gas to enter the booster chamber and a gas outlet to allow gas to exit the booster chamber;
a first rotor positioned within the booster chamber and adapted for rotation therein, the first rotor including a first shaft and at least two lobes having an outer surface that defines a first lobe profile; and
a second rotor positioned within the booster chamber and adapted for rotation therein, the second rotor including a second shaft and at least two lobes having an outer surface that defines a second lobe profile,
wherein the first and second rotors are formed from a metal including at least about 50% iron, about 20% to about 35% nickel, and about 10% to about 25% cobalt and having a coefficient of thermal expansion from about 1 (10 −6 in/in*K) to about 13 (10 −6 in/in*K), and wherein the outer surface of the first rotor and the outer surface of the second rotor each includes a coating including at least one of an abradable coating or a formable coating.
10. The vacuum booster assembly of claim 9 , wherein the coating includes at least two layers formed from two different materials.
11. The vacuum booster assembly of claim 9 , wherein a portion of the coating from the first and second rotors partially transfers onto a portion of the booster housing during operation of the vacuum booster assembly.
12. The vacuum booster assembly of claim 9 , including an operating clearance between the first and second rotors from about 0.003 inches to about 0.032 inches and an operating clearance between the first rotor and the housing from about 0.002 inches to about 0.025 inches.
13. The vacuum booster assembly of claim 9 , wherein the coating has a coefficient of friction from about 0.04μ to about 0.2μ.
14. The vacuum booster assembly of claim 9 , wherein the coating includes one or more of a PTFE, a graphite, or molybdenum disulfide.
15. A vacuum booster assembly comprising:
a booster housing defining a booster chamber, the booster housing formed to include a gas inlet for allowing gas to enter the booster chamber and a gas outlet to allow gas to exit the booster chamber;
a first rotor positioned within the booster chamber and adapted for rotation therein, the first rotor including a first shaft and at least two lobes having an outer surface that defines a first lobe profile; and
a second rotor positioned within the booster chamber and adapted for rotation therein, the second rotor including a second shaft and at least two lobes having an outer surface that defines a second lobe profile,
wherein the first and second rotors formed from metal having a coefficient of thermal expansion from about 1 (10 −6 in/in*K) to about 13 (10 −6 in/in*K), wherein an inner surface of the booster housing includes a coating including at least one of an abradable coating or a formable coating, and wherein a portion of the coating has a thickness from about 0.001 inches to about 0.025 inches and a surface roughness from about 125 Ra to about 1000 Ra.
16. The vacuum booster assembly of claim 15 , wherein the coefficient of thermal expansion of the first and second rotors is from about 6 (10 −6 in/in*K) to about 11 (10 −6 in/in*K), and wherein the portion of the coating has a thickness from about 0.001 inches to about 0.006 inches.
17. The vacuum booster assembly of claim 15 , wherein the portion of the coating from the housing partially transfers onto a portion of the rotors during operation of the vacuum booster assembly.